US20090155084A1 - Wind blade joint bonding grid - Google Patents
Wind blade joint bonding grid Download PDFInfo
- Publication number
- US20090155084A1 US20090155084A1 US11/955,728 US95572807A US2009155084A1 US 20090155084 A1 US20090155084 A1 US 20090155084A1 US 95572807 A US95572807 A US 95572807A US 2009155084 A1 US2009155084 A1 US 2009155084A1
- Authority
- US
- United States
- Prior art keywords
- wind turbine
- adhesive
- turbine blade
- grid
- segment
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000000853 adhesive Substances 0.000 claims abstract description 71
- 230000001070 adhesive effect Effects 0.000 claims abstract description 71
- 238000009826 distribution Methods 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims abstract description 17
- 238000010438 heat treatment Methods 0.000 claims description 12
- 230000013011 mating Effects 0.000 description 16
- 238000005304 joining Methods 0.000 description 7
- 238000001723 curing Methods 0.000 description 4
- 238000002347 injection Methods 0.000 description 4
- 239000007924 injection Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000002131 composite material Substances 0.000 description 3
- 239000004800 polyvinyl chloride Substances 0.000 description 3
- 239000004801 Chlorinated PVC Substances 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 2
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical compound COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 2
- 229920000457 chlorinated polyvinyl chloride Polymers 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 229920001567 vinyl ester resin Polymers 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 240000007182 Ochroma pyramidale Species 0.000 description 1
- 239000004676 acrylonitrile butadiene styrene Substances 0.000 description 1
- 238000013006 addition curing Methods 0.000 description 1
- 239000004840 adhesive resin Substances 0.000 description 1
- 229920006223 adhesive resin Polymers 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 125000000484 butyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 150000002825 nitriles Chemical class 0.000 description 1
- 229920001084 poly(chloroprene) Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 238000003908 quality control method Methods 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/52—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
- B29C65/54—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/114—Single butt joints
- B29C66/1142—Single butt to butt joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
- B29C66/1162—Single bevel to bevel joints, e.g. mitre joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
- B29C66/543—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles joining more than two hollow-preforms to form said hollow articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/52—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
- B29C65/54—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts
- B29C65/542—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts by injection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
- B29L2031/085—Wind turbine blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/20—Manufacture essentially without removing material
- F05B2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/302—Segmented or sectional blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
Definitions
- the present invention is directed to elongated airfoils for use with wind turbines and methods for fabricating elongated airfoils for wind turbines.
- the present invention is directed to segmented wind turbine blades and methods for making large, elongated wind turbine blades.
- a wind turbine includes a rotor having multiple wind turbine blades.
- the wind turbine blades are elongated airfoils configured to provide rotational forces in response to wind.
- the rotor is mounted to a housing or nacelle, which is positioned on top of a truss or tubular tower.
- Utility grade wind turbines i.e., wind turbines designed to provide electrical power to a utility grid
- the wind turbines are typically mounted on towers that are at least 60 meters in height.
- Wind turbine blades may be very large and may require fabrication in two or more pieces. Segmented components provide ease of transportation but require joining of the segments together by bonding in order to fabricate the full turbine blade. The components may be joined together by adhesive or interlocking structure, but conventional joining techniques fail to provide sufficient bonding strength or sufficient durability between sections during wind turbine operation. In addition, known interlocking systems and/or bonding systems require heavy and/or expensive components that result in undesirable weight in the assembled wind turbine blade.
- a first aspect of the present invention includes a method and system for assembling large wind turbine blades that includes providing a plurality of wind turbine blade segments.
- An adhesive distribution arrangement is disposed on a surface of at least one of the plurality of the wind turbine blade segments.
- the adhesive distribution arrangement includes a bonding grid having a plurality of adhesive distribution openings.
- the wind turbine blade segments are directed together and sufficient adhesive is provided to the bonding grid to substantially fill an area between the wind turbine segments.
- the adhesive is then cured to form a bonded joint, the bonding grid being incorporated into the bonded joint.
- the arrangement includes a bonding grid having a port for receiving adhesive and a frame, the bonding grid being configured to deliver adhesive to a plurality of adhesive distribution openings.
- the distribution openings are configured to distribute adhesive onto one or more surfaces of a wind turbine blade segment.
- Still another aspect of the present invention includes a segmented wind turbine blade.
- the segmented wind turbine blade includes a first wind turbine blade segment and a second wind turbine blade segment.
- the first wind turbine blade segment is joined to the second wind turbine blade segment.
- a bonding grid disposed between adjacent surfaces of the first wind turbine blade segment and the second wind turbine blade segment.
- the bonding grid includes a frame having a plurality of cells disposed therein, where the cells are substantially filled cured adhesive. The distribution of adhesive is substantially uniform across the adjacent surfaces.
- the bonding grid provides controlled temperature and distribution of adhesive, and provides a quality control to validate the filling of the cavity.
- bonding grid provides a means of controlling the space between joined components to provide strong and uniform junctions between segments.
- Still another advantage is that the adhesive is distributed substantially uniformly across the bonding grid allowing for the formation of a strong uniform joint.
- segmented wind turbine blades may be shipped at a substantially reduced cost and easily assembled on-site.
- Still another advantage is that the method and system of the disclosure enables bonding in a wide variety of environments.
- FIG. 1 shows a side elevational view of a wind turbine according to an embodiment of the present disclosure.
- FIG. 2 shows a top perspective view of a wind turbine blade according to an embodiment of the present disclosure.
- FIG. 3 shows a crossectional view of a wind turbine blade take in direction 3 - 3 of FIG. 2 .
- FIG. 4 shows a top perspective view of wind turbine blade segments configured to be joined together according to an embodiment of the present disclosure.
- FIG. 5 shows a cross-sectional view of two wind turbine blade segments being directed together according to an embodiment of the present disclosure.
- FIG. 6 shows a top view of a bonding grid according to an embodiment of the present disclosure.
- FIG. 7 shows a cross-sectional view taken in direction 7 - 7 of FIG. 6 .
- FIG. 8 shows a cross-sectional view taken in direction 8 - 8 of FIG. 6 .
- FIG. 9 shows a cross-sectional view of two wind turbine blade segments being directed together with a bonding grid according to an embodiment of the present disclosure.
- FIG. 10 shows a top view of a wind turbine segment having a bonding grid disposed thereon according to an embodiment of the present disclosure.
- FIG. 11 shows a top perspective view of wind turbine blade segments configured to be joined together with a bonding grid disposed on surfaces of one wind turbine blade segment according to an embodiment of the present disclosure.
- FIG. 12 shows a top perspective view of wind turbine blade segments configured to be joined together with a bonding grid disposed on surfaces of two wind turbine blade segments according to an embodiment of the present disclosure.
- FIG. 1 shows a wind turbine 100 having a nacelle 102 housing a generator (not shown in FIG. 1 ).
- Nacelle 102 is a housing mounted atop a tower 104 , only a portion of which is shown in FIG. 1 .
- the height of tower 104 is selected based upon factors and conditions known in the art, and may extend to heights up to 60 meters or more.
- the wind turbine 100 may be installed on any terrain providing access to areas having desirable wind conditions. The terrain may vary greatly and may include, but is not limited to, mountainous terrain or off-shore locations.
- Wind turbine 100 also comprises a rotor 106 that includes one or more rotor blades 108 attached to a rotating hub 110 .
- wind turbine 100 illustrated in FIG. 1 includes three rotor blades 108 , there are no specific limits on the number of rotor blades 108 required by the present disclosure.
- FIG. 2 illustrates a turbine blade 108 according to an embodiment of the present disclosure having a leading edge 201 and a trailing edge 203 .
- the turbine blade 108 includes an airfoil portion 205 extending from the tip 207 to the root 209 , which is connectable to the hub 110 of the wind turbine.
- the blade includes a bonded joint 211 dividing a first segment 213 of the blade 108 from the second portion of the blade 108 .
- the first segment 213 and the second segment 215 are segments of the blade 108 , which are assembled together to provide a complete blade 108 .
- segment it is meant that the wind turbine blade 108 is divided into a plurality of components that, when assembled together, form a complete blade 108 .
- FIG. 2 shows a blade 108 having two segments, the disclosure is not limited to two segments. For example, blade 108 may be divided into any number of segments including three or more segments.
- FIG. 3 illustrates a cross-sectional view taken in direction 3 - 3 of the wind turbine blade 108 of FIG. 2 .
- FIG. 3 is a cross-section of a wind turbine blade taken along line 3 - 3 of FIG. 2 .
- the wind turbine blade 108 includes a first shell portion 301 and a second shell portion 302 , which are each adhesively or otherwise bonded to a spar cap 304 .
- the first shell portion 301 and the second shell portion 302 may be a unitary component.
- the spar cap 304 may be adhesively or otherwise bonded to the shear webs 303 .
- the spar cap 304 and the second shell portion 302 are adhesively or otherwise bonded.
- the shear web 303 , the spar cap 304 and the first and second shell portions 301 , 302 may adhered using an adhesive or other suitable joining structure.
- An outer skin 305 or coating may be applied to the outer surfaces of the blade 108 to provide additional structural support and to aid in aerodynamic performance.
- other structures known in the art for wind turbine blade 108 design such as stiffeners, fasteners or other hardware or structures may be present in the blade 108 .
- Other arrangements of shear web 303 and spar cap 304 may be provided including varied geometries of support.
- the shear web 303 and spar cap 304 may be arranged into a box geometry, and “I” geometry, a “T” geometry or any other suitable geometry that provides internal support between the first shell portion 301 and the second shell portion 302 . Further still, the shear web 303 may be arranged as shown and described in the modular interlocking blade configuration in U.S. Patent Publication US2007/0140858 to Bakhuis et al., which is herein incorporated by reference in its entirety.
- FIG. 4 shows a top perspective view of wind turbine blade segments configured to be joined together according to an embodiment of the present disclosure.
- first segment 213 includes a protrusion 401 extending from of the airfoil portion 205 .
- Protrusion 401 is an extension from the airfoil portion 205 that has a geometry configured to mate a mating cavity 403 of second segment 215 .
- the first mating edge 405 of the first segment 213 contacts or is in close proximity to the second mating edge 407 of the second segment.
- Protrusion 401 and mating cavity 403 are not limited to the arrangement or geometry shown and may include features such as splines, latches, grooves or other features to assist in alignment or inconnection.
- the length of the protrusion 401 and the depth of the mating cavity 403 are not limited any may include any arrangement that permits the joining together of the first segment 213 and the second segment 215 through an adhesive joint.
- the protrusion 401 and mating cavity 403 may be separate structures from the shear web 303 or may be integrated into the shear web 303 .
- the construction of the protrusion 401 and mating cavity 403 may be any suitable construction for use with wind turbine blades 108 and may include composite materials or reinforcing materials, such as glass or carbon fiber reinforced composites, polyvinyl chloride (PVC) or balsa core, with epoxy or vinyl ester resin and having hardware such as bolts and alignment pins.
- PVC polyvinyl chloride
- the protrusion 401 and the mating cavity 403 preferably include a tapered geometry (see e.g. FIG. 5 ) wherein the tapered geometry includes an angled geometry.
- the protrusion 401 preferably includes a decreasing cross-sectional area as the protrusion 401 extends from the airfoil portion 205 .
- the mating cavity 403 includes an increasing cross-sectional area from the interior to the second mating edge 407 .
- FIG. 5 shows a cross-sectional view of two wind turbine blade segments 213 , 215 being directed together according to an embodiment of the present disclosure.
- the protrusion 401 and the mating cavity 403 have corresponding geometries that permit mating.
- FIG. 5 shows a tapered surface
- the mating geometries are not so limited and may include any geometry that permits mating and allows the joining of the first segment 213 to the second segment 215 .
- the tampered surface shown in FIG. 5 is merely schematic and not limited to the taper shown.
- a bonding grid 601 may be used.
- FIG. 6 shows a top view of a bonding grid 601 according to an embodiment of the present disclosure.
- the bonding grid 601 includes a substantially rectangular frame 603 surrounding a plurality of conduits 605 arranged into a grid geometry.
- the conduits 605 are arranged to form a plurality of cells 607 .
- the cells 607 define a space into which adhesive may be distributed.
- the size and geometry of the cells 607 are not limited to the size and geometry shown and may be selected based upon the type of adhesive used, the size of the segments being joined, or other factors that affect the uniformity of adhesive distribution.
- the conduits 605 include opening 609 arranged along the edges of the cells 607 .
- the openings 609 are configured to permit the injection of adhesive into the space defined by cell 607 .
- the adhesive is permitted to contact any surfaces in contact with the frame 603 and/or the conduits 605 .
- surfaces of each of the first segment 213 and the second segment 215 are in contacted with adhesive provided to cell 607 .
- vents 611 that permit the escape of gas or air and allow the substantially complete filling of the cells 607 with adhesive.
- the vents 611 may be monitored to determine whether adhesive is present and the cells are substantially filled.
- vents 611 may be provided with vacuum or reduced pressure to assist in the distribution of the adhesive.
- a port 613 may be provided at any suitable location along the frame 603 in order to allow the injections of adhesive into the bonding grid 601 .
- the port 613 may be any structure capable of receiving adhesive and may include an extension or protrusion that permits the injection of adhesive when the first segment 213 and second segment are brought together (see e.g., FIG. 9 ).
- Adhesives suitable for use with the bonding grid includes any adhesive compositions known in the art for connecting composite materials. Suitable adhesive compositions include, but are not limited to, epoxy, polyester, methylacrylate, vinylester or other adhesive resin. Bonding grid 601 further includes an optional heating element 615 arranged along conduit 605 .
- FIG. 7 shows a cross-sectional view of frame 603 taken in direction 7 - 7 of FIG. 6 .
- frame 603 preferably includes a seal 701 arranged along the edges to permit containment of adhesive within cells 607 .
- the seal may be a foam, rubber, polymer or other compressible or deformable material suitable for providing sealing of adhesive, while being conformable to a surface of the first segment 213 and/or the second segment 215 .
- the frame 603 desirably provides a uniform spacing between the first segment 213 and the second segment 215 across the bonding joint 211 by maintaining a frame thickness along the length of the bonding grid 601 .
- the frame 603 can be made from polyvinyl chloride (PVC), acrylonitrile butadiene styrene (ABS) and/or chlorinated polyvinyl chloride (CPVC).
- PVC polyvinyl chloride
- ABS acrylonitrile butadiene styrene
- CPVC chlorin
- FIG. 8 shows a cross-sectional view taken in direction 8 - 8 of FIG. 6 .
- the conduit 605 includes an opening 609 arranged on edges thereof.
- the conduit may be a pipe, hose or other suitable structure capable of conveying adhesive.
- the conduit 605 is preferably a lightweight, inexpensive semi-rigid material capable of maintaining strength when incorporated into the assembled wind turbine blade 108 .
- the conduit 605 maybe a butyl, nitrile, neoprene and/or polyvinyl chloride piping material.
- the openings 609 are not limited to mere openings and may be configured in any suitable manner to distribute adhesive.
- the openings 609 may be configured to a nozzle geometry to permit efficient distribution of the resin.
- the conduit 605 may include an optional heating element 615 arranged along one or more edges of the conduit 605 .
- the heating element 615 may be utilized in low temperature ambient environments to maintain adhesive viscosity during injection or prevent freezing.
- heating element 615 may be utilized to assist or facilitate curing of the adhesive.
- the heating element 615 may be any suitable heating element.
- the heating element 615 is an electrically resistive heater that is connectable to an exterior electrical source.
- the present invention is not limited to the resistive wire/heater and may include fluid heating, chemical heating or any other type of heating that provides temperature control to the adhesive.
- An alternate approach includes combining the frame 603 with the conduit 605 by means of adding intermittent spacing structures to the conduit.
- the conduit 605 is flexible enough to provide the sealing function while spacers ensure a minimum gap.
- FIG. 9 shows a cross-sectional view of two wind turbine blade segments 213 , 215 being directed together with a bonding grid 601 according to an embodiment of the present disclosure.
- the bonding grid 601 is intermediate to the first segment 213 and the second segment 215 .
- the first segment 213 and the second segment 215 are brought into close proximity wherein the bonding grid 601 is configured to contact both the first segment 213 and second segment 215 .
- the bonding grid 601 is preferably disposed on a surface of one of the first segment 213 or the second segment 215 prior to bringing the segments together (see e.g., FIG. 10 ).
- FIG. 10 shows a top view of a wind turbine segment having a bonding grid 601 disposed thereon according to an embodiment of the present disclosure.
- the first mating edge 405 of the first segment 213 contacts or is in close proximity to the second mating edge 407 of the second segment, forming a substantially continuous surface on the outer surface of wind turbine blade 108 (see e.g., FIG. 2 ).
- the first segment 213 and second segment 215 are each in a sealed contact with the bonding grid by contacting and/or compressing the seal 701 of the frame 603 of the bonding grid 601 .
- Adhesive is provided to the bonding grid 601 via port 613 (see e.g., FIG. 6 ).
- the adhesive is distributed to cells 607 .
- the adhesive is provided until the cells 607 are substantially full. Once the adhesive is sufficiently distributed, the adhesive may be cured.
- “Cure”, “cured”, “curing” and grammatical variations thereof as utilized herein mean that the adhesive is permitted to dry and/or cross-link sufficiently to provide an adhesive bond. Curing may be at ambient temperatures or elevated temperatures. In addition curing may be in the presence or absence of a catalyst.
- the bonding grid 601 is preferably incorporated into the bonding joint and remains in place subsequent to curing.
- FIGS. 11 and 12 show alternate arrangements of the bonding grid 601 prior to joining the first segment 213 to the second segment 215 .
- FIG. 11 shows a top perspective view of wind turbine blade segments 213 , 215 configured to be joined together with a bonding grid 601 disposed on surfaces of one wind turbine blade segment 213 according to an embodiment of the present disclosure.
- FIG. 12 shows a top perspective view of wind turbine blade segments 213 , 215 configured to be joined together with a bonding grid 601 disposed on surfaces of two wind turbine blade segments according to an embodiment of the present disclosure.
- the present disclosure is not limited to the arrangement shown in FIGS.
- first segment 213 and/or second segment 215 may include disposing the bonding grid on one, two, three or more surfaces of either or both of first segment 213 and/or second segment 215 . Further, the bonding grid may be initially adhered to the surface of first segment 213 and/or second segment 215 prior to joining the first segment 213 to the second segment.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
Abstract
Description
- The present invention is directed to elongated airfoils for use with wind turbines and methods for fabricating elongated airfoils for wind turbines. In particular, the present invention is directed to segmented wind turbine blades and methods for making large, elongated wind turbine blades.
- Recently, wind turbines have received increased attention as environmentally safe and relatively inexpensive alternative energy sources. With this growing interest, considerable efforts have been made to develop wind turbines that are reliable and efficient.
- Generally, a wind turbine includes a rotor having multiple wind turbine blades. The wind turbine blades are elongated airfoils configured to provide rotational forces in response to wind. The rotor is mounted to a housing or nacelle, which is positioned on top of a truss or tubular tower. Utility grade wind turbines (i.e., wind turbines designed to provide electrical power to a utility grid) can have large rotors (e.g., 30 or more meters in length). In addition, the wind turbines are typically mounted on towers that are at least 60 meters in height.
- Wind turbine blades may be very large and may require fabrication in two or more pieces. Segmented components provide ease of transportation but require joining of the segments together by bonding in order to fabricate the full turbine blade. The components may be joined together by adhesive or interlocking structure, but conventional joining techniques fail to provide sufficient bonding strength or sufficient durability between sections during wind turbine operation. In addition, known interlocking systems and/or bonding systems require heavy and/or expensive components that result in undesirable weight in the assembled wind turbine blade.
- Further, due to the large size of the components and the necessity for a strong bond, good distribution of adhesive is required. Currently there is no method of system that provides sufficiently uniform distribution of adhesive to join wind turbine blade segments.
- What is needed is an improved method and system for fabricating large segmented wind turbine blades that includes durable and strong bonding joints that do not suffer from the drawbacks of known systems.
- A first aspect of the present invention includes a method and system for assembling large wind turbine blades that includes providing a plurality of wind turbine blade segments. An adhesive distribution arrangement is disposed on a surface of at least one of the plurality of the wind turbine blade segments. The adhesive distribution arrangement includes a bonding grid having a plurality of adhesive distribution openings. The wind turbine blade segments are directed together and sufficient adhesive is provided to the bonding grid to substantially fill an area between the wind turbine segments. The adhesive is then cured to form a bonded joint, the bonding grid being incorporated into the bonded joint.
- Another aspect of the present invention includes an adhesive distribution arrangement for assembling large wind turbine blades. The arrangement includes a bonding grid having a port for receiving adhesive and a frame, the bonding grid being configured to deliver adhesive to a plurality of adhesive distribution openings. The distribution openings are configured to distribute adhesive onto one or more surfaces of a wind turbine blade segment.
- Still another aspect of the present invention includes a segmented wind turbine blade. The segmented wind turbine blade includes a first wind turbine blade segment and a second wind turbine blade segment. The first wind turbine blade segment is joined to the second wind turbine blade segment. A bonding grid disposed between adjacent surfaces of the first wind turbine blade segment and the second wind turbine blade segment. The bonding grid includes a frame having a plurality of cells disposed therein, where the cells are substantially filled cured adhesive. The distribution of adhesive is substantially uniform across the adjacent surfaces.
- One advantage of an embodiment is that the bonding grid provides controlled temperature and distribution of adhesive, and provides a quality control to validate the filling of the cavity.
- Another advantage is that the bonding grid provides a means of controlling the space between joined components to provide strong and uniform junctions between segments.
- Still another advantage is that the adhesive is distributed substantially uniformly across the bonding grid allowing for the formation of a strong uniform joint.
- Still another advantage is that the segmented wind turbine blades may be shipped at a substantially reduced cost and easily assembled on-site.
- Still another advantage is that the method and system of the disclosure enables bonding in a wide variety of environments.
- Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
-
FIG. 1 shows a side elevational view of a wind turbine according to an embodiment of the present disclosure. -
FIG. 2 shows a top perspective view of a wind turbine blade according to an embodiment of the present disclosure. -
FIG. 3 shows a crossectional view of a wind turbine blade take in direction 3-3 ofFIG. 2 . -
FIG. 4 shows a top perspective view of wind turbine blade segments configured to be joined together according to an embodiment of the present disclosure. -
FIG. 5 shows a cross-sectional view of two wind turbine blade segments being directed together according to an embodiment of the present disclosure. -
FIG. 6 shows a top view of a bonding grid according to an embodiment of the present disclosure. -
FIG. 7 shows a cross-sectional view taken in direction 7-7 ofFIG. 6 . -
FIG. 8 shows a cross-sectional view taken in direction 8-8 ofFIG. 6 . -
FIG. 9 shows a cross-sectional view of two wind turbine blade segments being directed together with a bonding grid according to an embodiment of the present disclosure. -
FIG. 10 shows a top view of a wind turbine segment having a bonding grid disposed thereon according to an embodiment of the present disclosure. -
FIG. 11 shows a top perspective view of wind turbine blade segments configured to be joined together with a bonding grid disposed on surfaces of one wind turbine blade segment according to an embodiment of the present disclosure. -
FIG. 12 shows a top perspective view of wind turbine blade segments configured to be joined together with a bonding grid disposed on surfaces of two wind turbine blade segments according to an embodiment of the present disclosure. - Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts.
-
FIG. 1 shows awind turbine 100 having anacelle 102 housing a generator (not shown inFIG. 1 ). Nacelle 102 is a housing mounted atop atower 104, only a portion of which is shown inFIG. 1 . The height oftower 104 is selected based upon factors and conditions known in the art, and may extend to heights up to 60 meters or more. Thewind turbine 100 may be installed on any terrain providing access to areas having desirable wind conditions. The terrain may vary greatly and may include, but is not limited to, mountainous terrain or off-shore locations.Wind turbine 100 also comprises arotor 106 that includes one ormore rotor blades 108 attached to a rotatinghub 110. Althoughwind turbine 100 illustrated inFIG. 1 includes threerotor blades 108, there are no specific limits on the number ofrotor blades 108 required by the present disclosure. -
FIG. 2 illustrates aturbine blade 108 according to an embodiment of the present disclosure having a leadingedge 201 and atrailing edge 203. Theturbine blade 108 includes anairfoil portion 205 extending from thetip 207 to theroot 209, which is connectable to thehub 110 of the wind turbine. The blade includes abonded joint 211 dividing afirst segment 213 of theblade 108 from the second portion of theblade 108. Thefirst segment 213 and thesecond segment 215 are segments of theblade 108, which are assembled together to provide acomplete blade 108. By segment, it is meant that thewind turbine blade 108 is divided into a plurality of components that, when assembled together, form acomplete blade 108. AlthoughFIG. 2 shows ablade 108 having two segments, the disclosure is not limited to two segments. For example,blade 108 may be divided into any number of segments including three or more segments. -
FIG. 3 illustrates a cross-sectional view taken in direction 3-3 of thewind turbine blade 108 ofFIG. 2 .FIG. 3 is a cross-section of a wind turbine blade taken along line 3-3 ofFIG. 2 . Thewind turbine blade 108 includes afirst shell portion 301 and asecond shell portion 302, which are each adhesively or otherwise bonded to aspar cap 304. In other embodiments, thefirst shell portion 301 and thesecond shell portion 302 may be a unitary component. Thespar cap 304 may be adhesively or otherwise bonded to theshear webs 303. In addition, thespar cap 304 and thesecond shell portion 302 are adhesively or otherwise bonded. Theshear web 303, thespar cap 304 and the first andsecond shell portions outer skin 305 or coating may be applied to the outer surfaces of theblade 108 to provide additional structural support and to aid in aerodynamic performance. In addition, other structures known in the art forwind turbine blade 108 design, such as stiffeners, fasteners or other hardware or structures may be present in theblade 108. Other arrangements ofshear web 303 andspar cap 304 may be provided including varied geometries of support. For example, theshear web 303 andspar cap 304 may be arranged into a box geometry, and “I” geometry, a “T” geometry or any other suitable geometry that provides internal support between thefirst shell portion 301 and thesecond shell portion 302. Further still, theshear web 303 may be arranged as shown and described in the modular interlocking blade configuration in U.S. Patent Publication US2007/0140858 to Bakhuis et al., which is herein incorporated by reference in its entirety. -
FIG. 4 shows a top perspective view of wind turbine blade segments configured to be joined together according to an embodiment of the present disclosure. As shown inFIG. 4 ,first segment 213 includes aprotrusion 401 extending from of theairfoil portion 205.Protrusion 401 is an extension from theairfoil portion 205 that has a geometry configured to mate amating cavity 403 ofsecond segment 215. When mated, thefirst mating edge 405 of thefirst segment 213 contacts or is in close proximity to thesecond mating edge 407 of the second segment.Protrusion 401 andmating cavity 403 are not limited to the arrangement or geometry shown and may include features such as splines, latches, grooves or other features to assist in alignment or inconnection. In addition, the length of theprotrusion 401 and the depth of themating cavity 403 are not limited any may include any arrangement that permits the joining together of thefirst segment 213 and thesecond segment 215 through an adhesive joint. Theprotrusion 401 andmating cavity 403 may be separate structures from theshear web 303 or may be integrated into theshear web 303. The construction of theprotrusion 401 andmating cavity 403 may be any suitable construction for use withwind turbine blades 108 and may include composite materials or reinforcing materials, such as glass or carbon fiber reinforced composites, polyvinyl chloride (PVC) or balsa core, with epoxy or vinyl ester resin and having hardware such as bolts and alignment pins. Theprotrusion 401 and themating cavity 403 preferably include a tapered geometry (see e.g.FIG. 5 ) wherein the tapered geometry includes an angled geometry. For example, theprotrusion 401 preferably includes a decreasing cross-sectional area as theprotrusion 401 extends from theairfoil portion 205. Correspondingly, themating cavity 403 includes an increasing cross-sectional area from the interior to thesecond mating edge 407. -
FIG. 5 shows a cross-sectional view of two windturbine blade segments protrusion 401 and themating cavity 403 have corresponding geometries that permit mating. AlthoughFIG. 5 shows a tapered surface, the mating geometries are not so limited and may include any geometry that permits mating and allows the joining of thefirst segment 213 to thesecond segment 215. Further, the tampered surface shown inFIG. 5 is merely schematic and not limited to the taper shown. In order to join thefirst segment 213 to the second segment 215 a bonding grid 601 (seeFIG. 6 ) may be used. -
FIG. 6 shows a top view of abonding grid 601 according to an embodiment of the present disclosure. As shown, thebonding grid 601 includes a substantiallyrectangular frame 603 surrounding a plurality ofconduits 605 arranged into a grid geometry. Theconduits 605 are arranged to form a plurality ofcells 607. Thecells 607 define a space into which adhesive may be distributed. The size and geometry of thecells 607 are not limited to the size and geometry shown and may be selected based upon the type of adhesive used, the size of the segments being joined, or other factors that affect the uniformity of adhesive distribution. Theconduits 605 include opening 609 arranged along the edges of thecells 607. Theopenings 609 are configured to permit the injection of adhesive into the space defined bycell 607. As thecell 607 is open, the adhesive is permitted to contact any surfaces in contact with theframe 603 and/or theconduits 605. For example, when thefirst segment 213 andsecond segment 215 are brought together (see e.g.,FIG. 9 ), surfaces of each of thefirst segment 213 and thesecond segment 215 are in contacted with adhesive provided tocell 607. - In addition to
openings 609, thecells 607 are arranged withvents 611 that permit the escape of gas or air and allow the substantially complete filling of thecells 607 with adhesive. In addition, in certain embodiments of the invention, thevents 611 may be monitored to determine whether adhesive is present and the cells are substantially filled. In addition, vents 611 may be provided with vacuum or reduced pressure to assist in the distribution of the adhesive. Aport 613 may be provided at any suitable location along theframe 603 in order to allow the injections of adhesive into thebonding grid 601. Theport 613 may be any structure capable of receiving adhesive and may include an extension or protrusion that permits the injection of adhesive when thefirst segment 213 and second segment are brought together (see e.g.,FIG. 9 ). Adhesives suitable for use with the bonding grid includes any adhesive compositions known in the art for connecting composite materials. Suitable adhesive compositions include, but are not limited to, epoxy, polyester, methylacrylate, vinylester or other adhesive resin.Bonding grid 601 further includes anoptional heating element 615 arranged alongconduit 605. -
FIG. 7 shows a cross-sectional view offrame 603 taken in direction 7-7 ofFIG. 6 . As is visible inFIG. 7 ,frame 603 preferably includes aseal 701 arranged along the edges to permit containment of adhesive withincells 607. The seal may be a foam, rubber, polymer or other compressible or deformable material suitable for providing sealing of adhesive, while being conformable to a surface of thefirst segment 213 and/or thesecond segment 215. Theframe 603 desirably provides a uniform spacing between thefirst segment 213 and thesecond segment 215 across the bonding joint 211 by maintaining a frame thickness along the length of thebonding grid 601. Theframe 603 can be made from polyvinyl chloride (PVC), acrylonitrile butadiene styrene (ABS) and/or chlorinated polyvinyl chloride (CPVC). -
FIG. 8 shows a cross-sectional view taken in direction 8-8 ofFIG. 6 . As shown inFIG. 8 , theconduit 605 includes anopening 609 arranged on edges thereof. The conduit may be a pipe, hose or other suitable structure capable of conveying adhesive. Theconduit 605 is preferably a lightweight, inexpensive semi-rigid material capable of maintaining strength when incorporated into the assembledwind turbine blade 108. For example, theconduit 605 maybe a butyl, nitrile, neoprene and/or polyvinyl chloride piping material. Theopenings 609 are not limited to mere openings and may be configured in any suitable manner to distribute adhesive. For example, theopenings 609 may be configured to a nozzle geometry to permit efficient distribution of the resin. In addition, theconduit 605 may include anoptional heating element 615 arranged along one or more edges of theconduit 605. Theheating element 615 may be utilized in low temperature ambient environments to maintain adhesive viscosity during injection or prevent freezing. In addition,heating element 615 may be utilized to assist or facilitate curing of the adhesive. Theheating element 615 may be any suitable heating element. In one embodiment, theheating element 615 is an electrically resistive heater that is connectable to an exterior electrical source. The present invention is not limited to the resistive wire/heater and may include fluid heating, chemical heating or any other type of heating that provides temperature control to the adhesive. An alternate approach includes combining theframe 603 with theconduit 605 by means of adding intermittent spacing structures to the conduit. In this embodiment, theconduit 605 is flexible enough to provide the sealing function while spacers ensure a minimum gap. -
FIG. 9 shows a cross-sectional view of two windturbine blade segments bonding grid 601 according to an embodiment of the present disclosure. Thebonding grid 601 is intermediate to thefirst segment 213 and thesecond segment 215. Thefirst segment 213 and thesecond segment 215 are brought into close proximity wherein thebonding grid 601 is configured to contact both thefirst segment 213 andsecond segment 215. Thebonding grid 601 is preferably disposed on a surface of one of thefirst segment 213 or thesecond segment 215 prior to bringing the segments together (see e.g.,FIG. 10 ).FIG. 10 shows a top view of a wind turbine segment having abonding grid 601 disposed thereon according to an embodiment of the present disclosure. When mated, thefirst mating edge 405 of thefirst segment 213 contacts or is in close proximity to thesecond mating edge 407 of the second segment, forming a substantially continuous surface on the outer surface of wind turbine blade 108 (see e.g.,FIG. 2 ). - In one embodiment, the
first segment 213 andsecond segment 215 are each in a sealed contact with the bonding grid by contacting and/or compressing theseal 701 of theframe 603 of thebonding grid 601. Adhesive is provided to thebonding grid 601 via port 613 (see e.g.,FIG. 6 ). The adhesive is distributed tocells 607. The adhesive is provided until thecells 607 are substantially full. Once the adhesive is sufficiently distributed, the adhesive may be cured. “Cure”, “cured”, “curing” and grammatical variations thereof as utilized herein mean that the adhesive is permitted to dry and/or cross-link sufficiently to provide an adhesive bond. Curing may be at ambient temperatures or elevated temperatures. In addition curing may be in the presence or absence of a catalyst. Thebonding grid 601 is preferably incorporated into the bonding joint and remains in place subsequent to curing. -
FIGS. 11 and 12 show alternate arrangements of thebonding grid 601 prior to joining thefirst segment 213 to thesecond segment 215.FIG. 11 shows a top perspective view of windturbine blade segments bonding grid 601 disposed on surfaces of one windturbine blade segment 213 according to an embodiment of the present disclosure.FIG. 12 shows a top perspective view of windturbine blade segments bonding grid 601 disposed on surfaces of two wind turbine blade segments according to an embodiment of the present disclosure. The present disclosure is not limited to the arrangement shown inFIGS. 11 and 12 , but may include disposing the bonding grid on one, two, three or more surfaces of either or both offirst segment 213 and/orsecond segment 215. Further, the bonding grid may be initially adhered to the surface offirst segment 213 and/orsecond segment 215 prior to joining thefirst segment 213 to the second segment. - While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (18)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/955,728 US8221085B2 (en) | 2007-12-13 | 2007-12-13 | Wind blade joint bonding grid |
DK200801727A DK177817B1 (en) | 2007-12-13 | 2008-12-08 | Wind turbine blade joint grille |
DE102008055513.4A DE102008055513B4 (en) | 2007-12-13 | 2008-12-11 | Joint bonding grid for wind turbine rotor blades |
CN2008101868020A CN101457781B (en) | 2007-12-13 | 2008-12-12 | Wind blade joint bonding grid |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/955,728 US8221085B2 (en) | 2007-12-13 | 2007-12-13 | Wind blade joint bonding grid |
Publications (2)
Publication Number | Publication Date |
---|---|
US20090155084A1 true US20090155084A1 (en) | 2009-06-18 |
US8221085B2 US8221085B2 (en) | 2012-07-17 |
Family
ID=40680240
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/955,728 Active 2031-05-16 US8221085B2 (en) | 2007-12-13 | 2007-12-13 | Wind blade joint bonding grid |
Country Status (4)
Country | Link |
---|---|
US (1) | US8221085B2 (en) |
CN (1) | CN101457781B (en) |
DE (1) | DE102008055513B4 (en) |
DK (1) | DK177817B1 (en) |
Cited By (84)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100310379A1 (en) * | 2007-12-21 | 2010-12-09 | General Electric Company | Structure and method for self-aligning rotor blade joints |
CN101979239A (en) * | 2010-10-22 | 2011-02-23 | 株洲时代新材料科技股份有限公司 | Method for adhering blades of megawatt wind turbine in die assembly |
US20110081248A1 (en) * | 2009-10-01 | 2011-04-07 | Vestas Wind Systems A/S | Wind Turbine Blade |
US7922454B1 (en) * | 2010-10-29 | 2011-04-12 | General Electric Company | Joint design for rotor blade segments of a wind turbine |
US20110091326A1 (en) * | 2008-05-07 | 2011-04-21 | Vestas Wind Systems A/S | Sectional Blade |
US20110123343A1 (en) * | 2009-11-24 | 2011-05-26 | Ronner David E | Wind turbine blade and methods, apparatus and materials for fabrication in the field |
US20110158788A1 (en) * | 2008-08-31 | 2011-06-30 | Vestas Wind Systems A/S | A sectional blade |
US20110171032A1 (en) * | 2008-06-20 | 2011-07-14 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements having geometrically well-defined joint surface portions |
US20110189025A1 (en) * | 2008-06-20 | 2011-08-04 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements comprising different materials |
GB2477847A (en) * | 2010-02-10 | 2011-08-17 | Albert Edward David Walters | Wind turbine blade with connecting elements |
WO2011098506A1 (en) * | 2010-02-10 | 2011-08-18 | Vestas Wind Systems A/S | A sectional blade |
US20110223028A1 (en) * | 2010-03-12 | 2011-09-15 | Jason Stege | Arrangement and method to retrofit a wind turbine |
WO2012031602A1 (en) * | 2010-09-09 | 2012-03-15 | Vestas Wind Systems A/S | Method for making a wind turbine blade including determining the thickness of a wind turbine blade component |
US8172539B2 (en) * | 2010-06-17 | 2012-05-08 | General Electric Company | Wind turbine rotor blade joint |
US20120134833A1 (en) * | 2011-12-19 | 2012-05-31 | General Electric Company | Root attachment for a rotor blade assembly |
US20120141286A1 (en) * | 2011-10-13 | 2012-06-07 | General Electric Company | Multi-segment wind turbine rotor blade with span-wise offset joints |
US20120219425A1 (en) * | 2011-02-24 | 2012-08-30 | Gamesa Innovation & Technology, S.L. | Wind turbine with multi-panel blade |
US20120237356A1 (en) * | 2009-09-23 | 2012-09-20 | Suzhou Red Maple Wind Blade Mould Co., Ltd. | Wind turbine blade and its producing method |
US20120269643A1 (en) * | 2009-12-02 | 2012-10-25 | Vestas Wind Systems A/S | Sectional wind turbine blade |
US20120301316A1 (en) * | 2011-05-24 | 2012-11-29 | Gamesa Innovation & Technology, S.L. | Bonding method for a wind turbine multi-panel blade |
WO2013084275A1 (en) | 2011-12-09 | 2013-06-13 | Mitsubishi Heavy Industries, Ltd. | Method of manufacturing a wind turbine blade and a wind turbine blade |
US20130216388A1 (en) * | 2012-02-20 | 2013-08-22 | General Electric Company | Box-shaped shear web for wind turbine blades and method of making |
US20130224032A1 (en) * | 2012-02-29 | 2013-08-29 | General Electric Company | Blade insert for a wind turbine rotor blade and related methods |
DE102011052841B4 (en) * | 2010-08-19 | 2013-11-21 | General Electric Co. | Rotor blade connection for a wind turbine |
WO2013178639A1 (en) * | 2012-05-30 | 2013-12-05 | youWINenergy GmbH | Blade assembly for a wind turbine rotor |
US20140140855A1 (en) * | 2010-05-24 | 2014-05-22 | Modular Wind Energy, Inc. | Segmented wind turbine blades with truss connection regions, and associated systems and methods |
EP2749765A1 (en) * | 2012-12-27 | 2014-07-02 | Siemens Aktiengesellschaft | Wind turbine rotor blade |
US20140286780A1 (en) * | 2011-08-05 | 2014-09-25 | Tecsis Tecnologia E Sistemas Avancados S.A. | Aerogenerator blade tip segment and method of assembly |
US8876483B2 (en) | 2010-01-14 | 2014-11-04 | Neptco, Inc. | Wind turbine rotor blade components and methods of making same |
US8899936B2 (en) | 2008-06-20 | 2014-12-02 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements having end portions extending transversely to an intermediate portion |
US8918997B2 (en) | 2011-10-13 | 2014-12-30 | General Electric Company | Method for assembling a multi-segment wind turbine rotor blade with span-wise offset joints |
US20150240780A1 (en) * | 2014-02-25 | 2015-08-27 | General Electric Company | Joint assembly for rotor blade segments of a wind turbine |
US9140235B2 (en) | 2012-08-22 | 2015-09-22 | General Electric Company | Variable length blade tip molds, tip assemblies and methods for manufacturing the same |
WO2016023555A1 (en) * | 2014-08-12 | 2016-02-18 | Vestas Wind Systems A/S | Improvements relating to wind turbine blade manufacture |
US9283726B2 (en) | 2013-11-07 | 2016-03-15 | Siemens Aktiengesellschaft | Wind turbine blade segment and method of manufacturing the wind turbine blade segment |
US9297357B2 (en) | 2013-04-04 | 2016-03-29 | General Electric Company | Blade insert for a wind turbine rotor blade |
EP3041665A1 (en) * | 2013-09-06 | 2016-07-13 | Wetzel Engineering, Inc. | Insert and method of attaching insert to structure |
US9394881B2 (en) | 2013-05-29 | 2016-07-19 | Siemens Aktiengesellschaft | Wind turbine blade and method of fabricating a wind turbine blade |
US20160281680A1 (en) * | 2013-11-05 | 2016-09-29 | Vestas Wind Systems A/S | Modular wind turbine rotor blade |
US9506452B2 (en) | 2013-08-28 | 2016-11-29 | General Electric Company | Method for installing a shear web insert within a segmented rotor blade assembly |
US9605651B2 (en) | 2013-12-04 | 2017-03-28 | General Electric Company | Spar assembly for a wind turbine rotor blade |
US9638166B2 (en) | 2009-06-30 | 2017-05-02 | Vestas Wind Systems A/S | Method of manufacturing a wind turbine blade comprising two members being joined by adhesion |
EP2867525B1 (en) * | 2012-05-30 | 2018-09-26 | youWINenergy GmbH | Apparatus for assembling blade sections |
US10137542B2 (en) | 2010-01-14 | 2018-11-27 | Senvion Gmbh | Wind turbine rotor blade components and machine for making same |
WO2019191046A1 (en) * | 2018-03-26 | 2019-10-03 | General Electric Company | Methods for joining blade components of rotor blades using printed grid structures |
WO2020028496A1 (en) * | 2018-08-03 | 2020-02-06 | General Electric Company | Process of assembling wind rotor blade segments by means of structural elements |
US10563636B2 (en) | 2017-08-07 | 2020-02-18 | General Electric Company | Joint assembly for a wind turbine rotor blade |
WO2020091791A1 (en) * | 2018-11-01 | 2020-05-07 | General Electric Company | Spacer material for reducing a bond gap between a beam structure and a blade shell of a segmented rotor blade |
WO2020122866A1 (en) * | 2018-12-11 | 2020-06-18 | General Electric Company | Beam structure for a segmented rotor blade having a transitioning shape |
WO2020131043A1 (en) * | 2018-12-19 | 2020-06-25 | General Electric Company | Jointed rotor blade having internal support structure with varying fiber orientation for pin reinforcement |
US10773464B2 (en) | 2017-11-21 | 2020-09-15 | General Electric Company | Method for manufacturing composite airfoils |
US10794359B2 (en) | 2018-09-24 | 2020-10-06 | General Electric Company | Jointed wind turbine blade with noise reduction tape |
US10821696B2 (en) | 2018-03-26 | 2020-11-03 | General Electric Company | Methods for manufacturing flatback airfoils for wind turbine rotor blades |
US10821652B2 (en) | 2017-11-21 | 2020-11-03 | General Electric Company | Vacuum forming mold assembly and method for creating a vacuum forming mold assembly |
US10830207B2 (en) | 2018-08-28 | 2020-11-10 | General Electric Company | Spar configuration for jointed wind turbine rotor blades |
US10830206B2 (en) | 2017-02-03 | 2020-11-10 | General Electric Company | Methods for manufacturing wind turbine rotor blades and components thereof |
EP3747639A1 (en) * | 2019-06-07 | 2020-12-09 | Siemens Gamesa Renewable Energy A/S | Method for manufacturing a wind turbine blade and wind turbine blade |
US10865769B2 (en) | 2017-11-21 | 2020-12-15 | General Electric Company | Methods for manufacturing wind turbine rotor blade panels having printed grid structures |
US10913216B2 (en) | 2017-11-21 | 2021-02-09 | General Electric Company | Methods for manufacturing wind turbine rotor blade panels having printed grid structures |
US10920745B2 (en) | 2017-11-21 | 2021-02-16 | General Electric Company | Wind turbine rotor blade components and methods of manufacturing the same |
US11035339B2 (en) | 2018-03-26 | 2021-06-15 | General Electric Company | Shear web assembly interconnected with additive manufactured components |
US11040503B2 (en) | 2017-11-21 | 2021-06-22 | General Electric Company | Apparatus for manufacturing composite airfoils |
US11098691B2 (en) | 2017-02-03 | 2021-08-24 | General Electric Company | Methods for manufacturing wind turbine rotor blades and components thereof |
US11149709B2 (en) | 2018-09-24 | 2021-10-19 | General Electric Company | Method to reduce noise and vibration in a jointed wind turbine blade, and associated wind turbine blade |
US11248582B2 (en) | 2017-11-21 | 2022-02-15 | General Electric Company | Multiple material combinations for printed reinforcement structures of rotor blades |
US11313346B2 (en) | 2018-06-08 | 2022-04-26 | Siemens Gamesa Renewable Energy A/S | Method of manufacturing wind turbine rotor blades |
US11390013B2 (en) | 2017-11-21 | 2022-07-19 | General Electric Company | Vacuum forming mold assembly and associated methods |
US11486352B2 (en) | 2018-11-01 | 2022-11-01 | General Electric Company | Scarf connection for a wind turbine rotor blade |
US11536246B2 (en) | 2018-11-01 | 2022-12-27 | General Electric Company | Span-wise extending pin for joining rotor blade segments |
US11572863B2 (en) | 2018-10-25 | 2023-02-07 | General Electric Company | Spar cap configuration for a jointed wind turbine blade |
US11572862B2 (en) * | 2017-12-25 | 2023-02-07 | Jiangsu Goldwind Science & Technology Co., Ltd. | Segmented blade, method for connecting segmented blades and wind power generator set |
US11614069B2 (en) | 2018-12-13 | 2023-03-28 | General Electric Company | Jointed rotor blade having a chord-wise extending pin supported via one or more structural members |
US11668277B2 (en) | 2018-11-01 | 2023-06-06 | General Electric Company | Wind turbine jointed rotor blade having a hollow chord-wise extending pin |
US11668275B2 (en) | 2017-11-21 | 2023-06-06 | General Electric Company | Methods for manufacturing an outer skin of a rotor blade |
US11680555B2 (en) | 2018-10-31 | 2023-06-20 | General Electric Company | Jointed wind turbine rotor blade having varying material combinations along its span for pin reinforcement |
US11780183B2 (en) | 2018-12-11 | 2023-10-10 | General Electric Company | Method for manufacturing a structural component of a blade segment for a rotor blade of a wind turbine |
US11795907B2 (en) | 2018-12-20 | 2023-10-24 | General Electric Company | Jointed wind turbine rotor blade having spar cap constructed of varying forms of materials along its span |
US11802542B2 (en) | 2018-11-01 | 2023-10-31 | General Electric Company | Method for installing and retaining a bushing in a bearing block of a rotor blade joint |
US11828264B2 (en) | 2018-11-01 | 2023-11-28 | General Electric Company | Compliant structures for jointed rotor blades |
US11840030B2 (en) | 2018-12-11 | 2023-12-12 | General Electric Company | Method for manufacturing a structural component of a blade segment for a rotor blade of a wind turbine |
US11878444B2 (en) | 2018-12-11 | 2024-01-23 | Ge Infrastructure Technology Llc | Method for manufacturing a hollow composite structure, particularly a spar beam for a wind turbine rotor blade, and an associated mandrel |
US11969959B2 (en) | 2018-12-11 | 2024-04-30 | Ge Infrastructure Technology Llc | Methods for manufacturing blade components for wind turbine rotor blades |
US12071923B2 (en) | 2018-12-20 | 2024-08-27 | Ge Infrastructure Technology Llc | Rotor blade segments secured together via internal support structures that define a variable size gap therebetween |
US12078143B2 (en) | 2019-10-09 | 2024-09-03 | Siemens Gamesa Renewable Energy A/S | Method for manufacturing a structural element of a wind turbine blade, method for manufacturing a wind turbine blade, structural element of a wind turbine blade and wind turbine blade |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DK3276162T3 (en) | 2008-12-05 | 2020-05-04 | Vestas Wind Sys As | EFFICIENT WINDOWS, WINDOWS AND ASSOCIATED SYSTEMS AND METHODS FOR MANUFACTURING, COLLECTION AND USE |
DK2357357T3 (en) * | 2009-10-01 | 2017-01-09 | Vestas Wind Sys As | The wind turbine blade |
CN101718250B (en) * | 2010-01-11 | 2011-11-09 | 华锐风电科技(集团)股份有限公司 | Sectional type wind wheel vanes of wind power generator set and assembly method thereof |
EP2368699B1 (en) | 2010-03-22 | 2018-11-21 | Vestas Wind Systems A/S | Method for manufacturing a blade spar for a windturbine |
DE102010015392B4 (en) * | 2010-04-19 | 2019-07-25 | Aero-Dynamik-Consult Gmbh | Connecting element for a rotor blade of a wind turbine |
DE102010040596A1 (en) * | 2010-09-10 | 2012-03-15 | Aloys Wobben | Removable rotor blade tip |
CN102011711B (en) * | 2010-12-06 | 2013-01-16 | 济南轨道交通装备有限责任公司 | Sectionalized-assembly type fan blade and manufacturing method thereof |
CN102700031A (en) * | 2011-03-28 | 2012-10-03 | 三一电气有限责任公司 | Heating method in wind turbine generator blade manufacturing process and heating device for manufacturing |
CN102200100A (en) * | 2011-06-02 | 2011-09-28 | 东方电气集团东方汽轮机有限公司 | Split-assembling-type blade of wind driven generator |
CN102734084A (en) * | 2012-06-26 | 2012-10-17 | 昆明理工峰潮科技有限公司 | Sectional blade of wind driven generator |
US9470205B2 (en) | 2013-03-13 | 2016-10-18 | Vestas Wind Systems A/S | Wind turbine blades with layered, multi-component spars, and associated systems and methods |
US20150369211A1 (en) * | 2014-06-19 | 2015-12-24 | General Electric Company | Wind blade tip joint |
DE102014118004B3 (en) | 2014-12-05 | 2016-03-31 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Rotor blade for wind turbines |
US10240896B2 (en) | 2015-03-12 | 2019-03-26 | Raytheon Company | Tube to bulkhead bonded joint design |
DE102016125452A1 (en) * | 2016-12-22 | 2018-06-28 | Wobben Properties Gmbh | Method for producing a wind turbine rotor blade and wind turbine rotor blade |
US10495058B2 (en) * | 2017-02-21 | 2019-12-03 | General Electric Company | Joint assembly for rotor blade segments of a wind turbine |
US11286908B2 (en) * | 2017-05-22 | 2022-03-29 | Lm Wind Power Us Technology Aps | Wind turbine blade and method of assembly of blade elements to form a wind turbine blade |
US10570879B2 (en) * | 2017-05-23 | 2020-02-25 | General Electric Company | Joint assembly for a wind turbine rotor blade with flanged bushings |
CN107795557B (en) * | 2017-11-10 | 2020-02-14 | 中国航发航空科技股份有限公司 | Adhesive forming device and adhesive method for engine rotor blade tenon |
CN111577528B (en) * | 2020-05-25 | 2021-03-26 | 湖南翰坤实业有限公司 | Wind power generation device and installation method of wind power generation blades |
CN111577529B (en) * | 2020-05-25 | 2021-04-30 | 湖南翰坤实业有限公司 | Wind power generation blade and installation method thereof |
EP3922446A1 (en) | 2020-06-12 | 2021-12-15 | Siemens Gamesa Renewable Energy A/S | Method for producing a wind turbine blade and wind turbine blade obtained thereby |
DK4050202T3 (en) * | 2021-02-24 | 2024-06-17 | Lm Wind Power As | A PROCEDURE FOR ASSEMBLY OF A WIND TURBINE BLADE |
DE102023112869B3 (en) | 2023-05-16 | 2024-08-22 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Segmented rotor blade for wind turbines |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3481810A (en) * | 1965-12-20 | 1969-12-02 | John C Waite | Method of manufacturing composite flooring material |
US4450038A (en) * | 1981-02-26 | 1984-05-22 | Aisin Seiki Kabushiki Kaisha | Hot air blast welding apparatus for thermoplastic parts |
US6282786B1 (en) * | 1999-08-16 | 2001-09-04 | General Electric Company | Method of making injection formed hybrid airfoil |
US6287080B1 (en) * | 1999-11-15 | 2001-09-11 | General Electric Company | Elastomeric formulation used in the construction of lightweight aircraft engine fan blades |
US6454536B1 (en) * | 2000-02-09 | 2002-09-24 | General Electric Company | Adhesion enhancers to promote bonds of improved strength between elastomers metals in lightweight aircraft fan blades |
US20070140858A1 (en) * | 2005-12-19 | 2007-06-21 | Bakhuis Jan W | Modularly constructed rotorblade and method for construction |
US20070243387A1 (en) * | 2006-04-13 | 2007-10-18 | Lin Wendy W | Dual cure resin composite system and method of manufacturing the same |
US7654799B2 (en) * | 2006-04-30 | 2010-02-02 | General Electric Company | Modular rotor blade for a wind turbine and method for assembling same |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2781551A1 (en) * | 2009-11-24 | 2011-06-03 | David E. Ronner | Wind turbine blade and methods, apparatus and materials for fabrication in the field |
US7922454B1 (en) * | 2010-10-29 | 2011-04-12 | General Electric Company | Joint design for rotor blade segments of a wind turbine |
-
2007
- 2007-12-13 US US11/955,728 patent/US8221085B2/en active Active
-
2008
- 2008-12-08 DK DK200801727A patent/DK177817B1/en active
- 2008-12-11 DE DE102008055513.4A patent/DE102008055513B4/en active Active
- 2008-12-12 CN CN2008101868020A patent/CN101457781B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3481810A (en) * | 1965-12-20 | 1969-12-02 | John C Waite | Method of manufacturing composite flooring material |
US4450038A (en) * | 1981-02-26 | 1984-05-22 | Aisin Seiki Kabushiki Kaisha | Hot air blast welding apparatus for thermoplastic parts |
US6282786B1 (en) * | 1999-08-16 | 2001-09-04 | General Electric Company | Method of making injection formed hybrid airfoil |
US6287080B1 (en) * | 1999-11-15 | 2001-09-11 | General Electric Company | Elastomeric formulation used in the construction of lightweight aircraft engine fan blades |
US6454536B1 (en) * | 2000-02-09 | 2002-09-24 | General Electric Company | Adhesion enhancers to promote bonds of improved strength between elastomers metals in lightweight aircraft fan blades |
US20070140858A1 (en) * | 2005-12-19 | 2007-06-21 | Bakhuis Jan W | Modularly constructed rotorblade and method for construction |
US20070243387A1 (en) * | 2006-04-13 | 2007-10-18 | Lin Wendy W | Dual cure resin composite system and method of manufacturing the same |
US7654799B2 (en) * | 2006-04-30 | 2010-02-02 | General Electric Company | Modular rotor blade for a wind turbine and method for assembling same |
Cited By (125)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100310379A1 (en) * | 2007-12-21 | 2010-12-09 | General Electric Company | Structure and method for self-aligning rotor blade joints |
US8167569B2 (en) * | 2007-12-21 | 2012-05-01 | General Electric Company | Structure and method for self-aligning rotor blade joints |
US20110091326A1 (en) * | 2008-05-07 | 2011-04-21 | Vestas Wind Systems A/S | Sectional Blade |
US9765756B2 (en) | 2008-05-07 | 2017-09-19 | Vestas Wind Systems A/S | Sectional blade |
US20110171032A1 (en) * | 2008-06-20 | 2011-07-14 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements having geometrically well-defined joint surface portions |
US8899936B2 (en) | 2008-06-20 | 2014-12-02 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements having end portions extending transversely to an intermediate portion |
US20110189025A1 (en) * | 2008-06-20 | 2011-08-04 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements comprising different materials |
US8777578B2 (en) | 2008-06-20 | 2014-07-15 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements having geometrically well-defined joint surface portions |
US8777579B2 (en) | 2008-06-20 | 2014-07-15 | Vestas Wind Systems A/S | Method of manufacturing a spar for a wind turbine from elements comprising different materials |
US20110158788A1 (en) * | 2008-08-31 | 2011-06-30 | Vestas Wind Systems A/S | A sectional blade |
US9638166B2 (en) | 2009-06-30 | 2017-05-02 | Vestas Wind Systems A/S | Method of manufacturing a wind turbine blade comprising two members being joined by adhesion |
US20120237356A1 (en) * | 2009-09-23 | 2012-09-20 | Suzhou Red Maple Wind Blade Mould Co., Ltd. | Wind turbine blade and its producing method |
US9291151B2 (en) * | 2009-09-23 | 2016-03-22 | Suzhou Red Maple Wind Blade Mould Co., Ltd. | Wind turbine blade and its producing method |
US20110081248A1 (en) * | 2009-10-01 | 2011-04-07 | Vestas Wind Systems A/S | Wind Turbine Blade |
US8177515B2 (en) | 2009-10-01 | 2012-05-15 | Vestas Wind Systems A/S | Wind turbine blade |
WO2011066279A3 (en) * | 2009-11-24 | 2011-11-24 | Ronner David E | Wind turbine blade and methods, apparatus and materials for fabrication in the field |
US20110123343A1 (en) * | 2009-11-24 | 2011-05-26 | Ronner David E | Wind turbine blade and methods, apparatus and materials for fabrication in the field |
US9388789B2 (en) * | 2009-12-02 | 2016-07-12 | Vestas Wind Systems A/S | Sectional wind turbine blade |
US20120269643A1 (en) * | 2009-12-02 | 2012-10-25 | Vestas Wind Systems A/S | Sectional wind turbine blade |
US9429140B2 (en) | 2010-01-14 | 2016-08-30 | Senvion Gmbh | Wind turbine rotor blade components and methods of making same |
US9945355B2 (en) | 2010-01-14 | 2018-04-17 | Senvion Gmbh | Wind turbine rotor blade components and methods of making same |
US8876483B2 (en) | 2010-01-14 | 2014-11-04 | Neptco, Inc. | Wind turbine rotor blade components and methods of making same |
US10137542B2 (en) | 2010-01-14 | 2018-11-27 | Senvion Gmbh | Wind turbine rotor blade components and machine for making same |
US9394882B2 (en) | 2010-01-14 | 2016-07-19 | Senvion Gmbh | Wind turbine rotor blade components and methods of making same |
US9255566B2 (en) | 2010-02-10 | 2016-02-09 | Vestas Wind Systems A/S | Sectional blade |
WO2011098506A1 (en) * | 2010-02-10 | 2011-08-18 | Vestas Wind Systems A/S | A sectional blade |
GB2477847A (en) * | 2010-02-10 | 2011-08-17 | Albert Edward David Walters | Wind turbine blade with connecting elements |
GB2477847B (en) * | 2010-02-10 | 2014-01-22 | Albert Edward David Walters | Improvements in or relating to methods of manufacture |
US20110223028A1 (en) * | 2010-03-12 | 2011-09-15 | Jason Stege | Arrangement and method to retrofit a wind turbine |
US9500179B2 (en) * | 2010-05-24 | 2016-11-22 | Vestas Wind Systems A/S | Segmented wind turbine blades with truss connection regions, and associated systems and methods |
US20140140855A1 (en) * | 2010-05-24 | 2014-05-22 | Modular Wind Energy, Inc. | Segmented wind turbine blades with truss connection regions, and associated systems and methods |
US8172539B2 (en) * | 2010-06-17 | 2012-05-08 | General Electric Company | Wind turbine rotor blade joint |
DK178744B1 (en) * | 2010-06-17 | 2016-12-19 | Gen Electric | Wind turbine rotor blade joint |
DE102011052841B4 (en) * | 2010-08-19 | 2013-11-21 | General Electric Co. | Rotor blade connection for a wind turbine |
WO2012031602A1 (en) * | 2010-09-09 | 2012-03-15 | Vestas Wind Systems A/S | Method for making a wind turbine blade including determining the thickness of a wind turbine blade component |
CN101979239A (en) * | 2010-10-22 | 2011-02-23 | 株洲时代新材料科技股份有限公司 | Method for adhering blades of megawatt wind turbine in die assembly |
US7922454B1 (en) * | 2010-10-29 | 2011-04-12 | General Electric Company | Joint design for rotor blade segments of a wind turbine |
DE102011054904B4 (en) * | 2010-10-29 | 2019-11-28 | General Electric Company | Connection design for rotor blade segments of a wind turbine |
US8967976B2 (en) * | 2011-02-24 | 2015-03-03 | Gamesa Innovation & Technology, S.L. | Wind turbine with multi-panel blade |
US20120219425A1 (en) * | 2011-02-24 | 2012-08-30 | Gamesa Innovation & Technology, S.L. | Wind turbine with multi-panel blade |
ES2398553A1 (en) * | 2011-02-24 | 2013-03-20 | Gamesa Innovation & Technology S.L. | An improved wind turbine multi-panel blade |
US20120301316A1 (en) * | 2011-05-24 | 2012-11-29 | Gamesa Innovation & Technology, S.L. | Bonding method for a wind turbine multi-panel blade |
EP2527128A3 (en) * | 2011-05-24 | 2013-03-06 | Gamesa Innovation & Technology, S.L. | A bonding method for a wind turbine multi-panel blade |
ES2399259A1 (en) * | 2011-05-24 | 2013-03-27 | Gamesa Innovation & Technology, S.L. | A bonding method for a wind turbine multi-panel blade |
US20140286780A1 (en) * | 2011-08-05 | 2014-09-25 | Tecsis Tecnologia E Sistemas Avancados S.A. | Aerogenerator blade tip segment and method of assembly |
US8918997B2 (en) | 2011-10-13 | 2014-12-30 | General Electric Company | Method for assembling a multi-segment wind turbine rotor blade with span-wise offset joints |
US20120141286A1 (en) * | 2011-10-13 | 2012-06-07 | General Electric Company | Multi-segment wind turbine rotor blade with span-wise offset joints |
US8517689B2 (en) * | 2011-10-13 | 2013-08-27 | General Electric Company | Multi-segment wind turbine rotor blade with span-wise offset joints |
WO2013084275A1 (en) | 2011-12-09 | 2013-06-13 | Mitsubishi Heavy Industries, Ltd. | Method of manufacturing a wind turbine blade and a wind turbine blade |
WO2013084390A1 (en) | 2011-12-09 | 2013-06-13 | Mitsubishi Heavy Industries, Ltd. | Method of manufacturing a wind turbine blade and a wind turbine blade |
US20120134833A1 (en) * | 2011-12-19 | 2012-05-31 | General Electric Company | Root attachment for a rotor blade assembly |
US8622707B2 (en) * | 2011-12-19 | 2014-01-07 | General Electric Company | Root attachment for a rotor blade assembly |
US20130216388A1 (en) * | 2012-02-20 | 2013-08-22 | General Electric Company | Box-shaped shear web for wind turbine blades and method of making |
US20130224032A1 (en) * | 2012-02-29 | 2013-08-29 | General Electric Company | Blade insert for a wind turbine rotor blade and related methods |
WO2013178639A1 (en) * | 2012-05-30 | 2013-12-05 | youWINenergy GmbH | Blade assembly for a wind turbine rotor |
EP2867525B1 (en) * | 2012-05-30 | 2018-09-26 | youWINenergy GmbH | Apparatus for assembling blade sections |
US9140235B2 (en) | 2012-08-22 | 2015-09-22 | General Electric Company | Variable length blade tip molds, tip assemblies and methods for manufacturing the same |
US9617973B2 (en) * | 2012-12-27 | 2017-04-11 | Siemens Aktiengesellschaft | Wind turbine rotor blade |
US20140186189A1 (en) * | 2012-12-27 | 2014-07-03 | Siemens Aktiengesellschaft | Wind turbine rotor blade |
EP2749765A1 (en) * | 2012-12-27 | 2014-07-02 | Siemens Aktiengesellschaft | Wind turbine rotor blade |
CN103899476A (en) * | 2012-12-27 | 2014-07-02 | 西门子公司 | Wind turbine rotor blade |
US9297357B2 (en) | 2013-04-04 | 2016-03-29 | General Electric Company | Blade insert for a wind turbine rotor blade |
US9394881B2 (en) | 2013-05-29 | 2016-07-19 | Siemens Aktiengesellschaft | Wind turbine blade and method of fabricating a wind turbine blade |
US9506452B2 (en) | 2013-08-28 | 2016-11-29 | General Electric Company | Method for installing a shear web insert within a segmented rotor blade assembly |
EP3041665A4 (en) * | 2013-09-06 | 2017-05-17 | We17 Llc | Insert and method of attaching insert to structure |
EP3041665A1 (en) * | 2013-09-06 | 2016-07-13 | Wetzel Engineering, Inc. | Insert and method of attaching insert to structure |
US11118561B2 (en) * | 2013-11-05 | 2021-09-14 | Vestas Wind Systems A/S | Modular wind turbine rotor blade |
US20160281680A1 (en) * | 2013-11-05 | 2016-09-29 | Vestas Wind Systems A/S | Modular wind turbine rotor blade |
US9283726B2 (en) | 2013-11-07 | 2016-03-15 | Siemens Aktiengesellschaft | Wind turbine blade segment and method of manufacturing the wind turbine blade segment |
US9605651B2 (en) | 2013-12-04 | 2017-03-28 | General Electric Company | Spar assembly for a wind turbine rotor blade |
US9790919B2 (en) * | 2014-02-25 | 2017-10-17 | General Electric Company | Joint assembly for rotor blade segments of a wind turbine |
US20150240780A1 (en) * | 2014-02-25 | 2015-08-27 | General Electric Company | Joint assembly for rotor blade segments of a wind turbine |
WO2016023555A1 (en) * | 2014-08-12 | 2016-02-18 | Vestas Wind Systems A/S | Improvements relating to wind turbine blade manufacture |
US10954915B2 (en) * | 2014-08-12 | 2021-03-23 | Vestas Wind Systems A/S | Wind turbine blade manufacture |
US11098691B2 (en) | 2017-02-03 | 2021-08-24 | General Electric Company | Methods for manufacturing wind turbine rotor blades and components thereof |
US10830206B2 (en) | 2017-02-03 | 2020-11-10 | General Electric Company | Methods for manufacturing wind turbine rotor blades and components thereof |
US10563636B2 (en) | 2017-08-07 | 2020-02-18 | General Electric Company | Joint assembly for a wind turbine rotor blade |
US10821652B2 (en) | 2017-11-21 | 2020-11-03 | General Electric Company | Vacuum forming mold assembly and method for creating a vacuum forming mold assembly |
US10773464B2 (en) | 2017-11-21 | 2020-09-15 | General Electric Company | Method for manufacturing composite airfoils |
US11248582B2 (en) | 2017-11-21 | 2022-02-15 | General Electric Company | Multiple material combinations for printed reinforcement structures of rotor blades |
US10920745B2 (en) | 2017-11-21 | 2021-02-16 | General Electric Company | Wind turbine rotor blade components and methods of manufacturing the same |
US11548246B2 (en) | 2017-11-21 | 2023-01-10 | General Electric Company | Apparatus for manufacturing composite airfoils |
US11040503B2 (en) | 2017-11-21 | 2021-06-22 | General Electric Company | Apparatus for manufacturing composite airfoils |
US11390013B2 (en) | 2017-11-21 | 2022-07-19 | General Electric Company | Vacuum forming mold assembly and associated methods |
US11668275B2 (en) | 2017-11-21 | 2023-06-06 | General Electric Company | Methods for manufacturing an outer skin of a rotor blade |
US10865769B2 (en) | 2017-11-21 | 2020-12-15 | General Electric Company | Methods for manufacturing wind turbine rotor blade panels having printed grid structures |
US10913216B2 (en) | 2017-11-21 | 2021-02-09 | General Electric Company | Methods for manufacturing wind turbine rotor blade panels having printed grid structures |
US11572862B2 (en) * | 2017-12-25 | 2023-02-07 | Jiangsu Goldwind Science & Technology Co., Ltd. | Segmented blade, method for connecting segmented blades and wind power generator set |
US11035339B2 (en) | 2018-03-26 | 2021-06-15 | General Electric Company | Shear web assembly interconnected with additive manufactured components |
US10821696B2 (en) | 2018-03-26 | 2020-11-03 | General Electric Company | Methods for manufacturing flatback airfoils for wind turbine rotor blades |
WO2019191046A1 (en) * | 2018-03-26 | 2019-10-03 | General Electric Company | Methods for joining blade components of rotor blades using printed grid structures |
US11313346B2 (en) | 2018-06-08 | 2022-04-26 | Siemens Gamesa Renewable Energy A/S | Method of manufacturing wind turbine rotor blades |
US11719222B2 (en) | 2018-08-03 | 2023-08-08 | General Electric Company | Method of joining wind turbine rotor blade segments via structural members |
WO2020028496A1 (en) * | 2018-08-03 | 2020-02-06 | General Electric Company | Process of assembling wind rotor blade segments by means of structural elements |
CN112513454A (en) * | 2018-08-03 | 2021-03-16 | 通用电气公司 | Method for assembling a wind rotor blade segment by means of structural elements |
JP2021535315A (en) * | 2018-08-28 | 2021-12-16 | ゼネラル・エレクトリック・カンパニイ | Spar configuration for joint wind turbine rotor blades |
JP7427656B2 (en) | 2018-08-28 | 2024-02-05 | ゼネラル エレクトリック レノバブレス エスパーニャ, エセ.エレ. | Spar configuration for joint wind turbine rotor blades |
US10830207B2 (en) | 2018-08-28 | 2020-11-10 | General Electric Company | Spar configuration for jointed wind turbine rotor blades |
US11149709B2 (en) | 2018-09-24 | 2021-10-19 | General Electric Company | Method to reduce noise and vibration in a jointed wind turbine blade, and associated wind turbine blade |
US10794359B2 (en) | 2018-09-24 | 2020-10-06 | General Electric Company | Jointed wind turbine blade with noise reduction tape |
US11572863B2 (en) | 2018-10-25 | 2023-02-07 | General Electric Company | Spar cap configuration for a jointed wind turbine blade |
US11680555B2 (en) | 2018-10-31 | 2023-06-20 | General Electric Company | Jointed wind turbine rotor blade having varying material combinations along its span for pin reinforcement |
US11802542B2 (en) | 2018-11-01 | 2023-10-31 | General Electric Company | Method for installing and retaining a bushing in a bearing block of a rotor blade joint |
US11828264B2 (en) | 2018-11-01 | 2023-11-28 | General Electric Company | Compliant structures for jointed rotor blades |
CN113286696A (en) * | 2018-11-01 | 2021-08-20 | 通用电气公司 | Spacer material for reducing a bond gap between a beam structure and a blade shell of a segmented rotor blade |
WO2020091791A1 (en) * | 2018-11-01 | 2020-05-07 | General Electric Company | Spacer material for reducing a bond gap between a beam structure and a blade shell of a segmented rotor blade |
US11486352B2 (en) | 2018-11-01 | 2022-11-01 | General Electric Company | Scarf connection for a wind turbine rotor blade |
US11536246B2 (en) | 2018-11-01 | 2022-12-27 | General Electric Company | Span-wise extending pin for joining rotor blade segments |
US11767819B2 (en) | 2018-11-01 | 2023-09-26 | General Electric Company | Spacer material, for reducing a bond gap between a beam structure and a blade shell of a segmented rotor blade |
US11668277B2 (en) | 2018-11-01 | 2023-06-06 | General Electric Company | Wind turbine jointed rotor blade having a hollow chord-wise extending pin |
WO2020122866A1 (en) * | 2018-12-11 | 2020-06-18 | General Electric Company | Beam structure for a segmented rotor blade having a transitioning shape |
US11969959B2 (en) | 2018-12-11 | 2024-04-30 | Ge Infrastructure Technology Llc | Methods for manufacturing blade components for wind turbine rotor blades |
US11542917B2 (en) | 2018-12-11 | 2023-01-03 | General Electric Company | Beam structure for a segmented rotor blade having a transitioning shape |
US11878444B2 (en) | 2018-12-11 | 2024-01-23 | Ge Infrastructure Technology Llc | Method for manufacturing a hollow composite structure, particularly a spar beam for a wind turbine rotor blade, and an associated mandrel |
US11780183B2 (en) | 2018-12-11 | 2023-10-10 | General Electric Company | Method for manufacturing a structural component of a blade segment for a rotor blade of a wind turbine |
US11840030B2 (en) | 2018-12-11 | 2023-12-12 | General Electric Company | Method for manufacturing a structural component of a blade segment for a rotor blade of a wind turbine |
US11614069B2 (en) | 2018-12-13 | 2023-03-28 | General Electric Company | Jointed rotor blade having a chord-wise extending pin supported via one or more structural members |
WO2020131043A1 (en) * | 2018-12-19 | 2020-06-25 | General Electric Company | Jointed rotor blade having internal support structure with varying fiber orientation for pin reinforcement |
US11802543B2 (en) | 2018-12-19 | 2023-10-31 | General Electric Company | Jointed rotor blade having internal support structure with varying fiber orientation for pin reinforcement |
CN113167217A (en) * | 2018-12-19 | 2021-07-23 | 通用电气公司 | Joined rotor blades having internal support structures with different fiber orientations for pin reinforcement |
US11795907B2 (en) | 2018-12-20 | 2023-10-24 | General Electric Company | Jointed wind turbine rotor blade having spar cap constructed of varying forms of materials along its span |
US12071923B2 (en) | 2018-12-20 | 2024-08-27 | Ge Infrastructure Technology Llc | Rotor blade segments secured together via internal support structures that define a variable size gap therebetween |
EP3747639A1 (en) * | 2019-06-07 | 2020-12-09 | Siemens Gamesa Renewable Energy A/S | Method for manufacturing a wind turbine blade and wind turbine blade |
WO2020244902A1 (en) * | 2019-06-07 | 2020-12-10 | Siemens Gamesa Renewable Energy A/S | Method for manufacturing a wind turbine blade and wind turbine blade |
US12078143B2 (en) | 2019-10-09 | 2024-09-03 | Siemens Gamesa Renewable Energy A/S | Method for manufacturing a structural element of a wind turbine blade, method for manufacturing a wind turbine blade, structural element of a wind turbine blade and wind turbine blade |
Also Published As
Publication number | Publication date |
---|---|
DE102008055513A1 (en) | 2009-06-18 |
US8221085B2 (en) | 2012-07-17 |
DE102008055513B4 (en) | 2016-03-24 |
DK200801727A (en) | 2009-06-14 |
CN101457781B (en) | 2013-03-06 |
CN101457781A (en) | 2009-06-17 |
DK177817B1 (en) | 2014-08-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8221085B2 (en) | Wind blade joint bonding grid | |
EP3112671B1 (en) | Modular wind turbine rotor blade | |
CN111108289B (en) | Injection method and apparatus for joining and repairing shear webs | |
US9500179B2 (en) | Segmented wind turbine blades with truss connection regions, and associated systems and methods | |
EP2577051B1 (en) | Segmented wind turbine blades with truss connection regions, and associated systems and methods | |
EP3112670B1 (en) | Method for assembling a modular wind turbine rotor blade | |
US9745954B2 (en) | Rotor blade joint assembly with multi-component shear web | |
US20140169978A1 (en) | Rotor blade assemblies and methods for assembling the same | |
US10760544B2 (en) | Sealing members for jointed rotor blade assemblies | |
WO2012123034A1 (en) | Arrangement to improve the surface of a wind turbine blade | |
DK201370472A (en) | Rotor blades with infused prefabricated shear webs and methods for making the same | |
BR112012033209B1 (en) | reduced notch composite joint | |
US11131290B2 (en) | Scarf connection for a wind turbine rotor blade | |
WO2018149526A1 (en) | A wind turbine blade, a wind turbine and a method for producing a wind turbine blade | |
EP3830412B1 (en) | Process of assembling wind rotor blade segments by means of structural elements | |
US10584678B2 (en) | Shear web for a wind turbine rotor blade | |
US20220010766A1 (en) | Scarf Connection for a Wind Turbine Rotor Blade | |
US11685081B2 (en) | Connection of mould parts | |
JP7210723B2 (en) | Spacer material for reducing coupling gap between segmented rotor blade beam structure and blade shell | |
US20210148328A1 (en) | Method of manufacturing a shell of a wind turbine blade having improved leading edge erosion protection, method for manufacturing the wind turbine blade, shell, wind turbine blade and wind turbine | |
EP4342659A1 (en) | Joining composite elements of wind turbine blades | |
US20240227337A1 (en) | A method of manufacturing a shell of a wind turbine blade | |
CN112912614A (en) | Method for mounting and retaining a bushing in a carrier block of a rotor blade joint |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: GENERAL ELECTRIC COMPANY, NEW YORK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:LIVINGSTON, JAMIE T;DRIVER, HOWARD;REEL/FRAME:020244/0350 Effective date: 20071212 |
|
FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
STCF | Information on status: patent grant |
Free format text: PATENTED CASE |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 8TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1552); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY Year of fee payment: 8 |
|
AS | Assignment |
Owner name: LM WIND POWER US TECHNOLOGY APS, DENMARK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GENERAL ELECTRIC COMPANY;REEL/FRAME:065531/0160 Effective date: 20231109 |
|
MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 12TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1553); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY Year of fee payment: 12 |
|
AS | Assignment |
Owner name: GE INFRASTRUCTURE TECHNOLOGY LLC, SOUTH CAROLINA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:LM WIND POWER US TECHNOLOGY APS;REEL/FRAME:066869/0770 Effective date: 20240322 |